Motion modeling and deployment control of a long tethered spacecraft system with an atmospheric sounder

被引:0
|
作者
机构
[1] Dong, Zhe
[2] Zabolotnov, Yuriy M.
[3] Wang, Changqing
关键词
Acoustic devices - Control theory - Aerodynamics - Tetherlines - Vibration control;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [1] Motion Modeling and Deployment Control of a Long Tethered Spacecraft System with an Atmospheric Sounder
    Dong, Zhe
    Zabolotnov, Yuriy M.
    Wang, Changqing
    ENGINEERING LETTERS, 2018, 26 (04)
  • [2] MODELING AND ANALYSIS OF DEPLOYMENT DYNAMICS OF A DISTRIBUTED ORBITAL TETHER SYSTEM WITH AN ATMOSPHERIC SOUNDER
    Dong, Zhe
    Zabolotnov, Y. M.
    Wang, Changqing
    THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017, 2017, 161 : 1051 - 1061
  • [3] Fractional-order sliding mode control for deployment of tethered spacecraft system
    Ma, Zhiqiang
    Zhu, Zheng H.
    Sun, Guanghui
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (13) : 4721 - 4734
  • [4] A unified energy-based control framework for tethered spacecraft deployment
    Junjie Kang
    Zheng H. Zhu
    Nonlinear Dynamics, 2019, 95 : 1117 - 1131
  • [5] A unified energy-based control framework for tethered spacecraft deployment
    Kang, Junjie
    Zhu, Zheng H.
    NONLINEAR DYNAMICS, 2019, 95 (02) : 1117 - 1131
  • [6] Underactuated attitude tracking control of tethered spacecraft for deployment and spin-up
    Tian, Haochang
    Li, Aijun
    Wang, Yu
    Wang, Changqing
    ADVANCES IN SPACE RESEARCH, 2023, 71 (11) : 4829 - 4842
  • [7] Experimental verification of chaotic attitude motion of tethered spacecraft system
    State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing
    210016, China
    Lixue Xuebao, 3 (503-512):
  • [8] Deployment Control of a Tethered Satellite System for Rendezvous with a Target
    Kojima, Hirohisa
    Taruoka, Yutaka
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2016, 59 (06) : 313 - 322
  • [9] Stability of Motion of a Tethered System when Towing Spacecraft with Propellant Outage
    Aslanov, V. S.
    Avramenko, A. A.
    MECHANICS OF SOLIDS, 2017, 52 (06) : 595 - 604
  • [10] Stability of Motion of a Tethered System when Towing Spacecraft with Propellant Outage
    V. S. Aslanov
    A. A. Avramenko
    Mechanics of Solids, 2017, 52 : 595 - 604